M7c16

14問 • 2ヶ月前

ユーザ名非公開

通報

問題一覧

The primary purpose of aircraft, weight and balance control, and safety. A secondary purpose is to

Achieve the utmost efficiency during flight

An overloaded aircraft

will need more runway to takeoff

Fore and aft limits of CG are

specified by the manufacturer

A moment arm is

negative if it is measured forward of the datum

A weight and balance schedule is normally retained in

the aircraft flight manual

the datum point on an aircraft, for measuring C of G position

could be anywhere on the aircraft

An aircraft which has its C of G forward of the forward limit

will have a longer take-off run.

The aircraft basic weight and centre of gravity position must be recorded on the following:

aircraft over 2730kg (6000 lbs) a Weight and Centre of Gravity Schedule

Aircraft below 5700kg not used for commercial air transport purpose are required to be

reweighed as required by the CAA

Aircraft exceeding 5700kg

must be reweighed after 2 years from manufacture then at periods not exceeding 5 years,

Unusable fuel also can be defined as

the fuel that cannot be pumped by the booster pump due to the low fuel level

Empty weight means

the basic weight plus unusable fuel plus oil.

The reaction is the load

at each separate weighing point.

Electrical or Electronic Weighing Equipment These type incorporate three or more weighing cells,

using metallic resistance elements or strain gauges, the resistance of which varies with change in length, due to elastic strain.

module 1 ch1

ユーザ名非公開 · 53問 · 11ヶ月前

module 1 ch1

53問 • 11ヶ月前

ユーザ名非公開

ユーザ名非公開 · 68問 · 11ヶ月前

68問 • 11ヶ月前

ユーザ名非公開

ユーザ名非公開 · 68問 · 11ヶ月前

m4 ch 2

m4 ch 2

m4 ch 3

m4 ch 3

m 4 ch 4

m 4 ch 4

M15c1

M15c1

M15c2

M15c2

M15c3

M15c3

M15c4

M15c4

M15c3

M15c3

M15c4

M15c4

M15c5

M15c5

M15c6

M15c6

M7c1

M7c1

M7c2

M7c2

M7c3

M7c3

M7c3

M7c3

M7c4

M7c4

問題一覧

The primary purpose of aircraft, weight and balance control, and safety. A secondary purpose is to

Achieve the utmost efficiency during flight

An overloaded aircraft

will need more runway to takeoff

Fore and aft limits of CG are

specified by the manufacturer

A moment arm is

negative if it is measured forward of the datum

A weight and balance schedule is normally retained in

the aircraft flight manual

the datum point on an aircraft, for measuring C of G position

could be anywhere on the aircraft

An aircraft which has its C of G forward of the forward limit

will have a longer take-off run.

The aircraft basic weight and centre of gravity position must be recorded on the following:

aircraft over 2730kg (6000 lbs) a Weight and Centre of Gravity Schedule

Aircraft below 5700kg not used for commercial air transport purpose are required to be

reweighed as required by the CAA

Aircraft exceeding 5700kg

must be reweighed after 2 years from manufacture then at periods not exceeding 5 years,

Unusable fuel also can be defined as

the fuel that cannot be pumped by the booster pump due to the low fuel level

Empty weight means

the basic weight plus unusable fuel plus oil.

The reaction is the load

at each separate weighing point.

Electrical or Electronic Weighing Equipment These type incorporate three or more weighing cells,

using metallic resistance elements or strain gauges, the resistance of which varies with change in length, due to elastic strain.